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Zenit-4M No. 16L

Re-entered 25 Jan 1971

Zenit-4M No. 16L (NORAD 4845, COSPAR 1971-001A) was a SU satellite that re-entered Earth's atmosphere on 25 Jan 1971, launched on 12 Jan 1971 on the Zenit-4M mission. It was operated by GUKOSR as part of the Zenit-4M programme. The spacecraft was built by TSKBE3 on the Zenit-4M bus, with a mass of 2,200 kg. Like most satellites in low orbits, it was gradually slowed by atmospheric drag until re-entry. Historical record from Orbital Radar's satellite archive, cross-referenced with the live satellite catalogue.

1971
launched
1971
re-entered
0
years on orbit
2,200
kg mass

Lifecycle

Launched12 Jan 1971 · on the Zenit-4M mission
Operational25 Jan 1971 · entered service
Retired25 Jan 1971 · end of operational service
Re-entered25 Jan 1971 · atmospheric re-entry — object destroyed

Specifications

NORAD ID4845
COSPAR1971-001A
TypeSatellite
OperatorGUKOSR
Country / StateSU
ManufacturerTSKBE3
BusZenit-4M
Mass2,200 kg
ProgrammeZenit-4M
CategoryIMG
OrbitLEO (LLEO/I)
Altitude203 × 273 km
Inclination65.0°

Frequently asked questions

What happened to Zenit-4M No. 16L?

Zenit-4M No. 16L re-entered Earth's atmosphere on 25 Jan 1971, ending a mission that began with its launch in 1971. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Zenit-4M No. 16L re-enter the atmosphere?

Zenit-4M No. 16L re-entered on 25 Jan 1971, according to Orbital Radar's historical catalogue records.

Who operated and built Zenit-4M No. 16L?

Zenit-4M No. 16L was operated by GUKOSR and built by TSKBE3 (SU).

Historical record from the Orbital Radar satellite archive. Sources & methodology: data sources. Accessed 2026-09-06.